Add to ORKGSpace transportation solid rocket motor systems; Shuttle derived heavy lift launch vehicles; advanced launch system (ALS) derived heavy lift launch vehicles; large launch solid booster vehicles are outlined. Performance capabilities and concept objectives are presented. Small launch vehicle concepts; enabling technologies; reusable flyback booster system; and high-performance solid motors for space are briefly described. This presentation is represented by viewgraphs
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
Goals of NASA's Advanced Booster Engineering Demonstration and/or Risk Reduction (ABEDRR) are to: (1...
The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable ...
The SLS booster combines proven technology from the past with cutting edge technology demonstrated b...
NASA's Journey to Mars has begun. Indicative of that challenge, this will be a multi-decadal effort ...
The National Aeronautics and Space Administration's (NASA's) Space Launch System (SLS) Program, mana...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
Two Solid Rocket Boosters provide the primary first stage thrust for the Space Shuttle. These Booste...
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
Technology development for low cost rocket boosters and estimates of total cost reduction obtainable...
The Advanced Launch System (ALS) is presented. The costs, reliability, capabilities, infrastructure ...
This report describes the preliminary design specifications for an Advanced Space Transportation Sys...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
Goals of NASA's Advanced Booster Engineering Demonstration and/or Risk Reduction (ABEDRR) are to: (1...
The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable ...
The SLS booster combines proven technology from the past with cutting edge technology demonstrated b...
NASA's Journey to Mars has begun. Indicative of that challenge, this will be a multi-decadal effort ...
The National Aeronautics and Space Administration's (NASA's) Space Launch System (SLS) Program, mana...
The factors affecting the choice of the 156 inch diameter, parallel burn, solid propellant rocket en...
The technical requirements for the solid propellant rocket engine to be used with the space shuttle ...
A conceptual design is presented for a carrier vehicle for an air launched space booster. This airpl...
Two Solid Rocket Boosters provide the primary first stage thrust for the Space Shuttle. These Booste...
The solid rocket motor failure database; current programs; and shortfalls of solid rocket propulsion...
An analysis and design effort was conducted as part of the study of solid rocket motor for a space s...
Technology development for low cost rocket boosters and estimates of total cost reduction obtainable...
The Advanced Launch System (ALS) is presented. The costs, reliability, capabilities, infrastructure ...
This report describes the preliminary design specifications for an Advanced Space Transportation Sys...
A technical analysis of the solid propellant rocket engines for use with the space shuttle is presen...
Goals of NASA's Advanced Booster Engineering Demonstration and/or Risk Reduction (ABEDRR) are to: (1...
The system includes reusable turbojet propelled booster vehicles releasably connected to a reusable ...